Medium multi-Purpose Helicopter Ka-62
(Equipment / Material)
Model Number: Ka-62
Condition: New
Location or Storage Country: Russia
Service Engineering Support: Yes
Warranty: Yes
Price: Call for price
Description:
The new medium multipurpose helicopter Ka-62 is designed using the latest global achievements in the aviation industry. Ka-62 meets Russian and international airworthiness standards (AP-29, CS-29, JAR-OPS3), operational rules for offshore operations, international standards for reliability, service life, flight safety, comfort conditions, technical operation and maintainability. Ka-62 is equipped with two Ardiden 3G turboshaft engines with a capacity of 1,776 hp manufactured by the French company SAFRAN HE. Due to the modular design and dual-channel electronic digital engine control system (FADEC), these engines are highly reliable, easy to use and have exceptionally low fuel consumption. The helicopter is equipped with a "glass cockpit" developed by Transas. Ka-62 is built according to a single-rotor scheme with a multi-blade tail rotor in the annular channel of the vertical tail unit. It has a five-bladed main rotor, a second hydraulic circuit, a high-capacity wheeled chassis, a reinforced fuselage structure and main unit mounting points, and shock-absorbing seats for the crew and passengers. It is planned that more than 50% of the rotor blades and airframe will be made of polymer composite materials. The Ka-62 is designed for cargo transportation, emergency medical care, aerial work and surveillance, it can be used in the oil and gas industry, for rescue operations and corporate needs. The Ka-62 has a wide range of applications: It can fly in the widest possible range of climatic and geographical conditions; Operating range of outside air temperatures from -50 ° C to + 50 ° C At temperatures down to -35 ° C, the helicopter is operated without heating the transmission units and engines; The Ka-62 is capable of flying in adverse weather conditions and in icing conditions; The Ka-62 can be operated from base airfields, oil platforms, and unprepared ground sites; the Ka-62 has the ability to be deployed autonomously and stored without a hangar.
Overview:
Flight performance characteristics
The speed limit is 310 km/h.
Cruising speed (max. continuous engine mode) - 290 km/h
Rate of climb - 14 m/s
Static ceiling outside the ground influence zone - 3200 m
Practical ceiling - 6100 m
Max. range with main fuel tanks - 700 km
Max. range with additional fuel tanks - 1135 km
Flight duration with standard fuel - 4 hours
Mass characteristics
Max. takeoff weight - 6800 kg
Max. payload on external sling - 2500 kg
Max. payload in transport cabin - 2000 kg
Engines
GT engines - 2xArdiden3G
Take-off power: 2x1776 hp
Maximum continuous mode - 2x1546 hp
Power in emergency mode - 1x1940 hp.
Dimensions
Length - 13470mm
Fuselage width - 1900 mm
Height - 4565 mm
Main rotor diameter - 13800 mm
Tail rotor diameter - 1400 mm
Chassis base - 5621 mm
Length of passenger cabin - 4100 mm
Passenger cabin width - 1740 mm
Height of passenger cabin - 1300
Capacity
Flight crew - 1-2
Passengers - up to 15